Presented is a procedure for improving the communication of requirements and specifications in the early design phases of an integrated helicopter/engine control system. The procedure is based on establishing a bound on a transfer matrix that relates blade cyclic and collective inputs to rotor speed variations. This bound becomes a new specification for the propulsion control system designer that embodies the mission-level performance goals of the helicopter. An example application of the procedure is provided for a Blackhawk/T700 system undergoing vertical accelerations from hover.


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    Titel :

    Integrated flight/propulsion control for helicopters


    Beteiligte:
    Rock, Stephen M. (Autor:in) / Neighbors, Ken (Autor:in)


    Erscheinungsdatum :

    01.07.1994



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Integrated Flight-Propulsion Control for Helicopters

    Rock, S.M. | Online Contents | 1994


    Integrated flight/propulsion control for helicopters

    Rock, S.M. / Neighbors, K. | Tema Archiv | 1994


    Integrated Flight/Propulsion Control for Helicopters

    Rock, S. M. / Neighbors, W. K. / American Helicopter Society | British Library Conference Proceedings | 1993



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